Development of Air Force Flight Safety Models. Volume 16. Feasibility of Adapting Model to Rotary Wing Aircraft; Example: UH-1N.

Abstract

The feasibility of applying the Flight Safety Prediction Technique to rotary wing aircraft is demonstrated through its application to the UH-1N helicopter. A complete safety model, compatible with the computer program used for a fixed wing aircraft, is presented. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1976
Accession Number
ADA054497

Entities

Organizations

  • ARINC

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Accidents
  • Air Force
  • Air Force Facilities
  • Aircraft Equipment
  • Aircrafts
  • Airframes
  • Computer Programming
  • Computer Programs
  • Feasibility Studies
  • Fixed Wing Aircraft
  • Flight
  • Functional Analysis
  • Helicopters
  • Plastic Explosives
  • Rotary Wing Aircraft
  • Terrorism
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Aerospace logistics and air mobility.
  • Software Engineering